A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation
By: Richard W. Barnwell.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.; Langley Research Center.
Series: NASA technical memorandum -- 81850.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1981
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 37
Subjects: Aerofoils -- Mathematical models.; Turbulent boundary layer -- Mathematical models.; Aerodynamics, Transonic.
Notes: "Langley Research Center."

"June 1981"--Cover.

Subject Category 02.

Includes bibliographical references.